Performance Data for the Piper PA-28 Archer
Piper PA-28 Archer · Performance Data
Overview
This document provides performance data specifically for the Piper PA-28 Archer. It is intended for pilots and aviation enthusiasts who require detailed information on the aircraft's capabilities, including speed, fuel consumption, climb rates, and other critical performance metrics. The data is essential for flight planning and operational safety, ensuring that pilots can make informed decisions based on the aircraft's performance under various conditions. The document serves as a reference for both new and experienced pilots, offering insights into the operational limits and performance characteristics of the PA-28 Archer.
- Maximum cruise speed: 138 knots
- Stall speed: 54 knots
- Climb rate: 730 feet per minute
- Maximum takeoff weight: 2,550 lbs
- Fuel consumption: 10 gallons per hour
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Aircraft Specifications
The Piper PA-28 Archer is a single-engine, low-wing aircraft with a seating capacity of four. It is powered by a Lycoming IO-360 engine, providing a maximum output of 180 horsepower. The aircraft has a wingspan of 36 feet and a length of 24 feet 2 inches, with a maximum takeoff weight of 2,550 lbs.
Performance Metrics
The PA-28 Archer has a maximum cruise speed of approximately 138 knots and a stall speed of 54 knots. The aircraft can climb at a rate of 730 feet per minute and has a service ceiling of 13,000 feet. The range of the aircraft is about 600 nautical miles with standard fuel reserves.
Weight and Balance
Proper weight and balance are crucial for safe flight operations. The document outlines the maximum weight limits, including useful load and baggage capacity. The maximum useful load is approximately 1,000 lbs, and the center of gravity limits are provided to ensure safe loading.
Fuel Consumption
The PA-28 Archer typically consumes about 10 gallons of fuel per hour during cruise flight. The fuel capacity is 50 gallons, with 48 gallons usable, allowing for extended flight durations.
Operational Limitations
The document details various operational limitations, including maximum crosswind component limits and turbulence penetration speeds. Pilots are advised to adhere to these limitations to ensure safety during flight.
Safety notes
- Ensure proper weight and balance before flight.
- Adhere to maximum crosswind component limits during takeoff and landing.